Mission System Study

Question 1

What are the ARF PME subsystems?

Answer 1

Power,
Foundation Equipment,
Enhanced Situational Awareness

Question 2

What does the Mission Control Power Switch do?

Answer 2

In the Off Position the PME does not receive power, in the Auto Position PME receives power.

In the Mission Control O-ride position, it allows operation of the PME on one generator.

Question 3

The PWR PNL AC segment light illuminates when?

Answer 3

Bus Cross Tie Switch is in the Auto/On position and both mission inverters fail.

Buss Cross Tie is in the Off position and either 3 Phase inverter fails.

Question 4

What does the WOW OVERRIDE light indicate?

Answer 4

Weight on Wheels Override switch is enabled allowing the Data Link to be operated on the ground.

Question 5

ESA OT light indicates?

Answer 5

Illuminates to indicate an OT (over-temperature) fault condition on either the ESA-R or ESA-P chassis.

Question 6

The LINK KG HOLD light illuminates to indicate?

Answer 6

The Data Link is holding cipher key data when the aircraft’s wheels are down.

Question 7

The Foundation Equipment consists of the following?

Answer 7

Mission Radios, INS/GPS, CDU, PFR and Status Panel

Question 8

What is the LN100G?

Answer 8

It is a versatile Inertial Navigation System/Global Positioning System (INS/GPS) capable of performing high-accuracy navigation while supplying sensor stability for location needs.

Question 9

The CDU 7000 provides?

Answer 9

The maintenance interface to the LN-100G (INS/GPS), the cockpit radios, the Mission Control Panel, and the Aircraft Avionics BUS DC (avionics power).

The option for the maintainer and aircraft crew to initiate a BIT on the LN-100G, Mission Radios, and the Mission Control Panel, as well as the CDU itself.

Question 10

What does the Precision Frequency Reference Unit provide?

Answer 10

It is the central resource for TIMING in the Guardrail system.

Question 11

Which of the following is NOT a function of the Status Panel?

A. Is where one can Zeroize the PME
B. Displays the POD temperatures
C. Tail number of the aircraft is set
D. Manual Data Link steering is conducted

Answer 11

d. Manual Data Link steering is conducted.

Question 12

Will the Status Panel illuminate some of the same faults that show up on the Mission Panel?

Answer 12

Yes, that is True

Question 13

How many mission radios are connected thru the CDU to the cockpit FMS?

Answer 13

2 (ARC 201 FM and ARC 164 UHF)

Question 14

Name the High level Guardrail Components.

Answer 14

ARF PME, IADL, TCDL, OGS, TST, TMET, MOF/JOIO

Question 15

ARF PME consists of ____ sets of equipment

Answer 15

5

ARF PME consists of 5 sets of equipment

Question 16

Where is the AEB mission prepared, planned, conducted and concluded?

Answer 16

MOF/Back Hall

Question 17

What is the mission of the AEBs?

Answer 17

The Aerial Exploitation Battalion (AEB) complements organic collection operations by providing intelligence to commanders by conducting multi-disciplined intelligence operations.

Question 18

What are the three location systems employed in the RC-12X? (Direction Finding)

Answer 18

X-Midas, CHAALS, HBC

Question 19

_____ is the heart of the Intercept system?

Answer 19

ESA

Question 20

True or False

X-Midas determines location by using Lines of Position and CHAALS determines geo-location using TDOA?

Answer 20

True

Question 21

Which of the following is not a consideration for track planning?

A. Altitude vs Range
B. Political Boundaries
C. Line-of-Sight
D. Time of Day

Answer 21

D. Time of Day

Question 22

What is the max depression angle from aircraft to target?

Answer 22

10 degrees

Question 23

The Status Panel and PRU are located on which rack?

Answer 23

A4

Question 24

Most of your Foundation Equipment is located on which rack?

Answer 24

A1